View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 69087U 26145.24938203 +.00000000 +00000-0 +32690-4 0 00006
2 69087 88.9864 344.2378 0002594 165.1979 194.9289 14.21989121 04
| Epoch (UTC): | 25 May 2026 05:59:06 |
| Eccentricity: | 0.0002594 |
| inclination: | 88.9864° |
| perigee height: | 817 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 344.2378° |
| argument of perigee: | 165.1979° |
| revolutions per day: | 14.21989121 |
| mean anomaly at epoch: | 194.9289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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